The nonlinear aeroelastic characteristics of a folding wing with cubic stiffness

Engineering

• Coefficient Matrix 100%
• Aerodynamics 50%
• Initial Condition 50%
• Aerodynamic Model 50%
• Lattice Method 50%
• Lagrange Equation 50%
• Constraint Equation 50%
• Model Structure 50%
• Influence Coefficient 50%
• Laplace Domain 50%